Experimental investigation on a high subsonic compressor cascade flow
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference27 articles.
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3. Kang S, Hirsch CH. Three dimensional flow in a linear compressor cascade at design conditions. New York: ASME; 1991. Report No.: ASME GT1991-114.
4. Development of hub corner stall and its influence on the performance of axial compressor blade rows;Hah;J Turbomach,1999
5. 3D transonic flow in a compressor cascade with shock-induced corner stall;Weber;J Turbomach,2002
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